View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65880U 26145.14370226 +.00000000 +00000-0 +45655-3 0 00001
2 65880 53.1599 298.8646 0001012 77.8292 282.2824 15.34409084 09
| Epoch (UTC): | 25 May 2026 03:26:55 |
| Eccentricity: | 0.0001012 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 298.8646° |
| argument of perigee: | 77.8292° |
| revolutions per day: | 15.34409084 |
| mean anomaly at epoch: | 282.2824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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